#
# #FileType= strain_life #DataType= fitted #TIMEcol= 0 #Name= PolyPhenyleneSulfide #Name= GlassFiber_Fitted #Name= polymer_composite # #Copyright (C) 2011 Fatigue Design and Evaluation Comm. #This data file is free software; you can redistribute it and/or #modify it under the terms of the GNU General Public License as #published by the Free Software Foundation; either version 2 of the #licenseor (at your option) any later version. #This data file is distributed in the hope that it will be useful #but WITHOUT ANY WARRANTY; without even the implied warranty of #MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the #GNU General PUblic License for more details. #You should have received a copy of the GNU General PUblic License #along with this program; if notwrite to the Free Software #FoundationInc.59 Temple Place - Suite 330BostonMA 02111-1307USA #Try also their web site: http://www.gnu.org/copyleft/gpl.html # # Fitted data Curve! # PolyPhenylene Sulfide 40%(weight) E-Glass (Fibers 0.02mm mostly) # Injection molded into ASTM D638 Type I tensile spec. # Original testing done at R=0.1 Load control. # Ref.: J.F.Mandell, D.D.Huang, F.J.McGarry, "Fatigue of Glass and Carbon # Reinforced Engineering Thermoplastics," Polym. Composites, V2 N3 July, # 1981 pp.137-144. Data digitized manually from plots in Ref. # Converted to fully reversed results using Tensile stress-strain curve # and Neuber Product plot of sqrt(Smax*Sa). Be aware that this is not # optimum method of describing the curves. # #Stress_units= mpa #Strain_units= strain #E= 24500 mpa (Initial tensile modulus from digitized tens. curve ) #Note: E modulus reported to soften with cycles. Amount not reported # #Su= 180 mpa #eu= 0.0050 strain # strain at Ultimate #true_fracture_strain= 0.0131 #true_fracture_stress= 180. mpa # # Str_Ampl 2Nf Sts_Amp_mpa MeanSts PlsStrAmp InitialMod. NeubAmpl 0.013125 1 180.5 0 .00576 24500 240.9 0.004754 108 93.8 0 .00093 24500 104.5 0.003197 2344 79.1 0 0 24500 78.7 0.002743 11710 70.8 0 0 24500 69.0 0.0024 55000 63. 0 0 24500 60.9 0.00216 199744 57.0 0 0 24500 55.0 0.002031 577680 51.1 0 0 24500 50.4 0.001901 4000000 44.4 0 0 24500 45.4 #